Solar refraction device for heating industrial materials

ABSTRACT

Disclosed is a solar refraction device (“SRD”) for heating industrial materials in a heating container, having a bottom, with diffuse solar energy that impinges on an outside surface of the SRD and is refracted through the SRD. The SRD may include a lens array assembly and a plurality of lens panes attached to the lens array assembly. The lens array assembly may include an outside surface corresponding to the outside surface of the SRD, an inside surface, and a plurality of lens array sub-assemblies.

CROSS-REFERENCE TO RELATED APPLICATIONS

The present application claims priority from, and is a divisionalapplication of U.S. patent application Ser. No. 14/829,553 filed Aug.18, 2015, the contents of which is incorporated by reference herein intheir entirety.

FIELD OF THE DISCLOSURE

This invention is generally related to solar systems, and in particular,to solar systems utilized to melt industrial materials.

BACKGROUND

There is a need to improve the energy efficiency associated with heatingand/or melting industrial materials at industrial volumes. At present inthe United States (“US”), melting industrial materials entails a largequantity of energy with aluminum fabrication alone accounting for about30% of that energy consumption. An even greater amount of energy isrequired when recycled steel is added. As such, major US industries,especially those industries related to metal recycling and stockmaterial fabrication, occupy a major portion of the nation's totalenergy consumption. Therefore, for nearly every industry involved in theprocess of fabrication or recycling of existing materials, there is aneed for high amounts of energy to melt materials, heat the materials,or for other key stage, or stages, of the process.

In general, the two major problems with conventional heating (e.g.,known furnaces (also known as burners) utilize gas, induction, blast,and electric arc furnaces (“EAFs”)) are their dependence on limited andfossil fuels (e.g., coal, oil, and natural gas), as well as theinefficiencies in how they transfer the generated thermal energy to heata material. It is appreciated by those of ordinary skill in the art thatthese types of furnaces have significant energy losses during thethermal energy transfer process (i.e., the process of heating thefurnace and then utilizing that heat to melt or heat the material),which ultimately results in about 30 to 40% efficiency. This resultsgenerally because large amounts of energy input into a furnace does notdirectly translate to thermal energy. As an example in a blast furnace,requires massive quantities of input energy to raise its temperature toits operating temperature. In aluminum melting, for example, only about40% of the energy utilized by the furnace goes to actually melting thealuminum.

This problem is also similar for furnaces utilizing induction melting,which is done typically open to air. Electrical resistance furnaces(“ERTs”) that utilize the principle of indirect heating are capable ofutilizing about 40% of their input energy for melting but in practiceare only typically about 26% efficient because ERT furnaces typicallyexperience other energy losses that include heating the air and thenlosing hot air through ventilation conduction to the insulating liner ofthe furnace and losses of energy when opening the ERT furnace. As aresult, EAF furnaces require large quantities of electrical power andcan have adverse environmental effects. Additionally, in many EAFfurnaces additionally gas burners are typically utilized to assist inheat scrap metal to a temperature where the metal conducts electricityefficiently so as allow the EAF furnace to run properly. Moreover,another major issue with these types of furnaces is the large carboncost of the process where the amount of carbon dioxide output by thesesystems. Unfortunately, their continued use is largely due to therelatively cheap cost of current sources of fuel.

Attempts to address and solve these problems utilizing “green energy”(i.e., renewable energy sources) have yet to materialize. Known uses ofsolar energy are not capable of addressing or solving these problemsbecause known solar technologies are limited in their capacity, windowof operation, and overall efficiency when capturing solar energy andtransferring it into a usable fashion. Specifically, known solar systemshave a number of inefficiencies in how they utilize solar energy toeither heat an object or generate electricity. These solar cells placedon solar panels utilize photovoltaic cells to convert solar energyimpinging on the solar cell into electricity. Common modernly usedcrystalline silicon solar cells output on average about 18% energyconversion due to losses of heat and the electricity transfer within thesolar cells.

In addition to solar cells, modern solar systems also include systemsthat heat objects, such as water pipes for example, that transfer theresulting heat energy to other objects for heating those objects orgenerating electricity through movement of, for example, water throughthe pipes to a turbine. Moreover, another problem with solar energy isthat it is not concentrated enough in any given area to use on anindustrial scale or it requires a system in place to utilize the energyin a process which converts it to useable electricity.

Attempts to solve these problems have includes using solar reflectorsystems to attempt to reflect and focus energy into a small area thatmay either generate power with a solar cell, heat water to generateelectricity through a turbine, or heat a small crucible containing somematerial in a small furnace. However, even with the use of reflectors,the resulting system still do not have high efficiency. The ones theutilize solar cells still only have 18% efficiency. The ones that heatwater still have the same thermal loses as the non-reflector solarheating systems. Additionally, the small furnaces lose energy fromhaving to heat a crucible. Moreover, all of these solar reflectorsystems lose energy from transferring energy to additional components inthe system and from reflection angle losses. Furthermore, some of thesesystems are stationary in a way that does not allow them to follow theSun and, therefore, limits the amount of time that they may operate. Asa result, without a change to modern solar energy capability, solarenergy cannot currently compete on a commercial scale and switching tosuch a technology would not be a cost benefit for most industries.

This is unfortunate because solar energy is a free resource which wouldover long periods of time, pay for itself in any application that canproperly capture and transfer solar energy into a usable fashion. Assuch, there is a need for solar energy capture system that is capable ofproducing a sufficient amount of energy for use in modern industrialprocesses that include heating or melting of industrial materials

SUMMARY

Disclosed is a solar refraction device (“SRD”) for heating industrialmaterials in a heating container, having a bottom, with diffuse solarenergy that impinges on an outside surface of the SRD and is refractedthrough the SRD. The SRD may include a lens array assembly and aplurality of lens panes attached to the lens array assembly. The lensarray assembly may include an outside surface corresponding to theoutside surface of the SRD, an inside surface, and a plurality of lensarray sub-assemblies. A sub-plurality of lens panes of the plurality oflens panes may be attached to a corresponding lens array sub-assembly ofthe plurality of lens array sub-assemblies. Moreover, each lens arraysub-assembly has a convex shape and may be configured to have a focallength corresponding to the lens array sub-assembly which results in thelens array assembly having a plurality of focal lengths.

As an example of operation, the SRD is configured to perform a methodthat includes refracting impinging solar energy on the SRD through thelens array assembly having the plurality of lens array sub-assemblies.The refracted solar energy is then focused onto a plurality of focalpoints, where each focal point corresponds to a lens array sub-assemblyof the plurality of lens array sub-assemblies. Utilizing the pluralityof focal points, the process then creates a heating area within theheating container. The process then heats the industrial material withinthe heating container at the heating area utilizing the focusedrefracted solar energy.

Also disclosed is a method for fabricating the SRD. The method includesdetermining the type and amount of industrial material to be melted anddetermining an amount of energy needed to melt the industrial material.An array size of a lens array assembly is then determined for producingthe previously determined amount of energy, where the lens arrayassembly is configured to refract solar light impinging on the lensarray assembly to the industrial material. The method then includesdetermining a focal length of the lens array assembly, assembling asupport frame to support the lens array assembly, and assembling thelens array assembly.

Other devices, apparatus, systems, methods, features and advantages ofthe invention will be or will become apparent to one with skill in theart upon examination of the following figures and detailed description.It is intended that all such additional systems, methods, features andadvantages be included within this description, be within the scope ofthe invention, and be protected by the accompanying claims.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention may be better understood by referring to the followingfigures. The components in the figures are not necessarily to scale,emphasis instead being placed upon illustrating the principles of theinvention. In the figures, like reference numerals designatecorresponding parts throughout the different views.

FIG. 1 is a perspective back-view of an example of an implementation ofa lens array assembly of a solar refraction device (“SRD”) in accordancewith the present disclosure.

FIG. 2 is a back-view of the lens array assembly shown in FIG. 1 inaccordance with the present disclosure.

FIG. 3 is a perspective back-view of an example of an implementation ofa lens array sub-assembly of the lens array assembly shown in FIGS. 1and 2 in accordance with the present disclosure.

FIG. 4 is a perspective back-view of an example of an implementation ofa single column array of lens panes of the lens array sub-assembly shownin FIGS. 1, 2, and 3 in accordance with the present disclosure.

FIG. 5A is a system view of an example of implementation of adiffracting convex lens.

FIG. 5B is a system view of the single column array of lens panes shownin FIG. 4 in accordance with the present disclosure.

FIG. 6 is a perspective side-view of the lens array sub-assembly shownin FIG. 3 in accordance with the present disclosure.

FIG. 7 is a perspective back-view of another example of animplementation of a lens array assembly of the SRD and a heatingcontainer in accordance with the present disclosure.

FIG. 8 is a system view of SRD shown in FIG. 7 in accordance with thepresent invention.

FIG. 9 is a perspective back-view of a plurality of SRDs, as shown inFIGS. 7 and 8, utilized to melt an industrial material in accordancewith the present disclosure.

FIG. 10 is a flowchart of an example of an implementation of processperformed by the SRD shown in FIGS. 1-9 in accordance with the presentdisclosure.

FIG. 11 is a flowchart of an example of an implementation of processperformed in fabricating the SRD in accordance with the presentdisclosure.

FIG. 12 is a system diagram of an example of an implementation of theSRD utilized for powering a turbine in accordance with the presentdisclosure.

DETAILED DESCRIPTION

A solar refraction device (“SRD”) for heating industrial materials in aheating container, having a bottom, with diffuse solar energy thatimpinges on an outside surface of the SRD and is refracted through theSRD is disclosed in accordance with the present disclosure. The SRD mayinclude a lens array assembly and a plurality of lens panes attached tothe lens array assembly. The lens array assembly may include an outsidesurface corresponding to the outside surface of the SRD, an insidesurface, and a plurality of lens array sub-assemblies. A sub-pluralityof lens panes of the plurality of lens panes may be attached to acorresponding lens array sub-assembly of the plurality of lens arraysub-assemblies. Moreover, each lens array sub-assembly has a convexshape and may be configured to have a focal length corresponding to thelens array sub-assembly which results in the lens array assembly havinga plurality of focal lengths.

As an example of operation in accordance with the present disclosure,the SRD is configured to perform a method that includes refractingimpinging solar energy (i.e., the solar energy that directly strikesand/or illuminates the SRD which may diffuse (i.e., spread) along anouter surface of the SRD) on the SRD through the lens array assemblyhaving the plurality of lens array sub-assemblies. The refracted solarenergy is then focused onto a plurality of focal points, where eachfocal point corresponds to a lens array sub-assembly of the plurality oflens array sub-assemblies. Utilizing the plurality of focal points, theprocess then creates a heating area within the heating container. Theprocess then heats the industrial material within the heating containerat the heating area utilizing the focused refracted solar energy.

Also disclosed is a method for fabricating the SRD in accordance withthe present disclosure. The method includes determining the type andamount of industrial material to be melted and determining an amount ofenergy needed to melt the industrial material. An array size of a lensarray assembly is then determined for producing the previouslydetermined amount of energy, where the lens array assembly is configuredto refract solar light impinging on the lens array assembly to theindustrial material. The method then includes determining a focal lengthof the lens array assembly, assembling a support frame to support thelens array assembly, and assembling the lens array assembly. In thisdisclosure the industrial material may include any type of materialutilized in an industrial, heating, or melting process. Examples ofindustrial material may include metallic industrial materials such as,for example, aluminum, steel, iron or other metals or alloys,non-metallic industrial material such as, for example, plastics or otherrecyclable non-metals, gasses, or liquids (such as, for example, water).

In FIG. 1, a perspective back-view of an example of an implementation ofa lens array assembly 100 of a solar refraction device (“SRD”) 102 isshown in accordance with the present disclosure. The SRD 102 includesthe lens array assembly 100 and a plurality of lens panes 104 attachedto the lens array assembly 100. In this example, the lens array assembly100 may include a support frame 106 constructed of a rigid material suchas, for example, a metal such as steel or aluminum or other rigidnon-metallic materials. The support frame 106 may include a plurality ofopenings that are configured to accept the plurality of lens panes 104,which are each configured to be attached to the lens array assembly 100.The support frame 106 is constructed of a rigid material that is strongenough to support the weight of, and stresses caused by, the pluralityof lens panes 104 placed within the plurality of opening in the supportframe 106 and capable of withstanding prolonged exposure in theenvironment to things such as, for example, electromagnetic radiation,thermal heat, and ultraviolent radiation without significantly degradingor warping. The lens array assembly 100 includes an outside surface 108that also corresponds to the outside surface of the SRD 102, an insidesurface (not shown), and a plurality of lens array sub-assemblies. Ingeneral, each lens array sub-assembly is a discrete panel of the lensarray assembly 100.

In this example, the lens array assembly 100 is shown having nine (9)lens array sub-assemblies 110, 112, 114, 116, 118, 120, 122, 124, and126. Each lens array sub-assembly is shown having a sub-plurality oflens panes (from the total plurality of lens panes 104) attached to thecorresponding lens array sub-assembly. As an example, part of a supportstructure 128 is also shown attached to one side of the lens arrayassembly 100. The support structure 128 may be attached to the supportframe 106 in a way that allows the support structure 128 to maintain thelens array assembly 100 at a predetermined distance from a heatingcontainer (not shown but described later) where the predetermineddistance is a distance that is based on the multiple focal lengths ofthe lens array assembly 100 (described in more detail later). Thesupport structure 128 may be connected to, or part of, a solar tracker(not shown), where the solar tracker is configured to move the supportstructure 128 (and the as the lens array assembly 100) in a manner thatmaintains a high amount of solar energy being refracted through the SRD102 and focused at a heating area. In this disclosure, a “high” amountof solar energy is considered enough solar energy for the SRD 102 tooperate according to the present description. Similar to the supportframe 106, the support structure 128 may also be constructed ofconstructed of a rigid material that is strong enough to support theweight of, and stresses caused by, the lens array assembly 100 an mayinclude metallic and non-metallic rigid materials. Furthermore, in thisexample, the lens array assembly 100 is shown to have athree-dimensional convex shape with each corresponding lens arraysub-assemblies 110, 112, 114, 116, 118, 120, 122, 124, and 126 alsobeing convex. The convex shape is approximately parabolic along thex-axis 130 and z-axis 132 and also along the y-axis 134 and z-axis 132.In an example of operation, the SRD 102 would refract diffuse solarenergy 136 (i.e., the impinging solar energy) that impinges on theoutside surface 108 (of both the SRD 102 and lens array assembly 100)through the SRD 102 resulting in a focused beam of refracted solarenergy 138 that is focused in a direction along the z-axis 132 away fromthe inside surface of the lens array assembly 100.

In this example, it is appreciated by those of ordinary skill in the artthat only nine (9) lens array sub-assemblies 110, 112, 114, 116, 118,120, 122, 124, and 126 have been shown in FIG. 1 for purpose ofillustration. However, the lens array assembly 100 may include more orless lens array sub-assemblies based on design and application of theSRD 102. As will be described later, in general each lens arraysub-assembly will produce a corresponding focused beam of refractedsolar energy that will have a focal length that corresponds to thespecific lens array sub-assembly. The resulting focal lengths from thedifferent lens array sub-assemblies may be different from each other sothat the combined focused beams of refracted solar energy (for each lensarray sub-assembly) combines to form the focused beam of refracted solarenergy 138 that produces a heating area (described later) that is notfocused to approximate point away (i.e., a single hot spot) from thelens array assembly 100 (described in more detail later).

From the detail in FIG. 1, in this example, the SRD 102 is shown to havean octagon two-dimensional convex shaped lens array assembly 100.Additionally, the lens array assembly 100 is shown to have five (5)rectangular shaped two-dimensional convex lens array sub-assemblies 110,112, 114, 116, and 118 and four (4) triangular shaped two-dimensionalconvex lens array sub-assemblies 120, 122, 124, and 126. Moreover, eachrectangular shaped two-dimensional convex lens array sub-assemblies 110,112, 114, 116, and 118 is shown to have 8 by 8 (i.e., 64) lens panes (orplurality of openings for 64 lens panes) and each triangular shapedtwo-dimensional convex lens array sub-assemblies 120, 122, 124, and 126is shown to have 28 lens panes (or plurality of openings for 28 lenspanes) and eight (8) half-sized lens panes (or plurality of openings for8 half sized lens panes). This results in the SRD 102 having, in thisexample, a total of 432 lens panes and 32 half sized lens panes. Each ofthe lens panes of the plurality of lens panes 104 may be flat lens panesapproximating a parabolic shape in the corresponding lens arraysub-assembly based on the size and number of the discrete flat lenspanes in the lens array sub-assembly or actual convex shaped lens panes.Furthermore, each lens panes may be made from either glass, acrylic, orother similar media. Moreover, each lens pane may be a flat or slopelens pane or a Fresnel lens such that the SRD 102 may be assembled froma combination of flat lens panes, sloped panes, and Fresnel lenses. Ingeneral, the lens panes may be removable and interchangeable within thelens array assembly 100. Additionally, in order to make the SRD 102 moredynamic, individual controls (not shown) may be installed in sections ofthe lens array assembly 100 or each opening that is configured toreceive a lens pane in the lens array assembly 100 such that thecontrols may be able to adjust the position of the individual panes toadjust the focus of the SRD 102. Again, the octagon two-dimensionalconvex shape of the lens array assembly 100 is an example forillustration purposes and may be a different shaped based on the designof the lens array assembly 100.

Turning to FIG. 2, a back-view of the lens array assembly 100, shown inFIG. 1 along viewing plane A-A′ 140, is shown in accordance with thepresent disclosure. FIG. 2 better illustrates the relationship of theplurality of sub-assemblies 110, 112, 114, 116, 118, 120, 122, 124, and126 and plurality of lens panes 104 in relationship with the lens arrayassembly 100. As described earlier, in this example, the lens arrayassembly 100 has an octagon shape and includes five rectangular shapedlens array sub-assemblies 110, 112, 114, 116, and 118, respectively, andfour triangular shaped lens sub-assemblies 120, 122, 124, and 126,respectively. In this example, as described earlier, the fiverectangular shaped lens array sub-assemblies 110, 112, 114, 116, and 118include 64 lens panes designated by 200, 202, 204, 206, and 208,respectively. Similarly, the four triangular shaped lens arraysub-assemblies 120, 122, 124, and 126 include 28 lens panes designatedby 210, 212, 214, and 216, respectively, and 8 partial sized lens panes218, 220, 222, and 224, respectively. If the four triangular shaped lensarray sub-assemblies 120, 122, 124, and 126 are generally equivalent tohalf of a rectangular shaped lens array sub-assemblies, then the fourtriangular shaped lens array sub-assemblies 120, 122, 124, and 126 actas the equivalent of two rectangular shaped lens array sub-assemblies.In this case, the lens array assembly 100 may be described as having atotal of seven (7) rectangular shaped lens array sub-assemblies insteadof nine (9). As a result, the SRD 102 would have a total equivalent of448 lens panes attached to the lens array assembly 100.

In general, the amount of energy produced by the SRD 102 is directlyrelated to location where the SRD 102 will be utilized and the arraysize of the lens array assembly 100. The higher the concentration ofsunlight the higher the amount of energy that may be produced by the SRD102 for a given size of the lens array assembly 100. Specifically,according to the National Renewable Energy Laboratory (“NREL”) averagedata from 1998 to 2009, areas within the United States such as Arizonaand parts of California, Nevada, New Mexico, Colorado, and Hawaiireceive as an annual average over 7.5 Kilowatt hours (“KWh”) per squaremeter (m²) per day of concentrated solar power (“CSP”) that is availablefor use by solar systems.

Generally, the amount of solar energy which falls on the Earth in any acalendar year dwarfs the total energy output of all the world's fossilfuels used in world's industries. For example, the State of Kentuckyreceives about 3.75 kW/m² of solar energy per day from the Sun andhigher energy areas, such as Hawaii, receive about 5.75 kW/m² of solarenergy per day. Only a fraction of these totals are used for creatinguseable energy with the current solar cells because, current commonlyused solar cells generally only reach about 18% energy conversion due tolosses of heat, reflection angle, and electricity transfer.

As such, utilizing Hawaii as an example for melting aluminum, a 6 footby 6 foot (i.e., an area of about 4 m²) lens array sub-assembly 110,112, 114, 116, and 118 would be able to focus about 4 KWh of solarenergy such that the lens array assembly 100 would be able to focus atleast 28 KWh of solar energy taking into account the five (5)rectangular shaped lens array sub-assemblies 110, 112, 114, 116, and 118and four (4) triangular shaped lens array sub-assemblies 120, 122, 124,and 126. Assuming, 85% efficiency in this example, the SRD 102 would becapable of melting about 74 pounds of aluminum per hour.

In FIG. 3, a perspective back-view of an example of an implementation ofa lens array sub-assembly 300 of the lens array assembly 100 (shown inFIGS. 1 and 2) is shown in accordance with the present disclosure. Thelens array sub-assembly 300 is show including a support frame 302 andapproximately 36 lens panes 304 organized in six (6) rows and six (6)columns. The reason for only showing six (6) columns and rows in thisexample is for convenience of illustration since every lens pane 304 isbeing shown within a support frame of the lens array sub-assembly 300.The support frame is shown having a first side 306 and a second side308. In this example, the convex curvature of the first side 306 of thesupport frame is shown along the x-axis 310 and z-axis 312. Similarly,the convex curvature of the second side 308 of the support frame isshown along the y-axis 314 and z-axis 312. As described earlier, theconvex curvature may be approximately parabolic for both the first andsecond sides 306 and 308 of the support frame. If approximatelyparabolic, the lens array assembly 100 will produce a more focused beamof refracted solar energy 138 because in general a parabola is a specialcurve that has the mathematical relationship that any point along thecurve of a parabola is equidistant from a fixed point (mathematicallyreferred to as the focus of the parabola but not to be confused with theterms focus utilized in the present disclosure) within the curve of theparabola.

Additionally, in FIG. 3, the panes 304 of a first column 316 of panes304 is shown receiving diffuse solar energy and focusing 318 it to afocal point 320. More specifically, turning to FIG. 4, a perspectiveback-view of an example of an implementation of a single column array oflens panes 400 of the lens array sub-assembly shown 300 (shown in FIG.3) is shown in accordance with the present disclosure. In this example,the single column array of lens panes 400 includes six (6) lens panes402, 404, 406, 408, 410, and 412. As an example of operation, the singlecolumn array of lens panes 400 is configured to receive a portion 414 ofthe diffuse solar energy 136 that impinges on the outside surface of theSRD and refract that portion 414 through the lens panes 402, 404, 406,408, 410, and 412 to produce a focused beam 416 of solar energy that isfocused to focal point 418.

To further explain this example, in FIGS. 5A and 5B, system views of acontinuous diffracting convex lens 500 and of the single column array oflens panes 502 (shown in FIG. 4 cut along plane B-B′ 420) are shownalong a center line 504. In both examples, impinging diffuse solarenergy 506 is diffracted and focused 508 and 510 to focal points 512 and514, respectively. As a result, in operation, the discrete diffractingconvex lens created by the single column array of lens panes 502 focuses510 the diffracted solar energy to approximately the same focal point514 as the focal point 512 of the continuous diffracting convex lens500.

In FIG. 6, a perspective side-view of the lens array sub-assembly 600(shown in FIG. 3 as lens array sub-assembly 300) is shown in accordancewith the present disclosure. Unlike the FIG. 3, in FIG. 6, an example ofoperation is shown where the diffuse solar energy 602 impinges on theoutside surface 604 of the lens array sub-assembly 600 that includes theplurality of lens panes 606. The each lens pane of the plurality of lenspanes 606 then diffracts a portion of the diffuse solar energy 602 andall of the diffracted beams from the plurality of lens panes 606 arefocused 608 into a focal point 610 that is utilized to heat or melt anindustrial material (not shown). In this example, the focal length 612of the lens array sub-assembly 600 is shown as the distance between thefocal point 610 and a center-line 614 of the lens array sub-assembly600. This focal length 612 is based on the design of the lens arraysub-assembly 600. Turning back to FIGS. 1 and 2, it is noted that thereare multiple lens array sub-assemblies 110, 112, 114, 116, 118, 120,122, 124, and 126 that may each have their own corresponding focallength. Additionally, these multiple focal lengths may be equal or notequal based on the design of the SRD for heating or melting anindustrial material. By having different focal lengths or differentfocal points for each lens array sub-assembly 110, 112, 114, 116, 118,120, 122, 124, and 126, the lens array assembly 100 may be configured tofocus the diffused solar energy that is a small area instead on a point.This allows the SRD 102 to be configured to melt an industrial materialat a heating plane within a heating container by distributing the heatof the focused solar energy over a small area at the heating plane. Ifthe focused solar energy is not distributed over a small area, it maypotential burn through the industrial material and potentially damagethe heating container because at a single focused point the energy toointense to properly be controlled as a furnace.

Expanding on this in FIG. 7, a perspective back-view of another exampleof an implementation of a lens array assembly 700 of the SRD 702 isshown in accordance with the present disclosure. In this example, thelens array assembly 700 is shown having five (5) rectangular shaped lensarray sub-assemblies 704, 706, 708, 710, and 712, respectively.Additional triangular shaped lens array sub-assemblies may also be addedas described earlier, however, in this example only five (5) rectangularshaped lens array sub-assemblies 704, 706, 708, 710, and 712 are shownfor the purposed of illustration. In this example, the lens arrayassembly 700 is shown having five different focal lengths or focalpoints 714, 716, 718, 720, and 722 for the individual lens arraysub-assemblies 704, 706, 708, 710, and 712. The resulting focal pointsdefine the small heating area 724 in the heating container 726. Ingeneral, by not directing the refracted light into a single direction,the light may be focused onto the small heating area 724 that is smallenough to heat or even melt the industrial material in the heatingcontainer 726 while large enough to maintain the heated or meltedindustrial material at a desired temperature.

Additionally shown in this example is the support structure 128 that maybe supporting the lens array assembly 700. In this example, the heatingarea 724 is shown to be a predetermined distance 728 from the lens arrayassembly 700. Specifically, the predetermined distance 728 is thedistance 728 between a center-line 730 of the plane of the heating area724 and another center-line 732 of the lens array assembly 700. Thepredetermined distance 728 is generally related to the focal lengths ofthe individual lens array sub-assemblies 704, 706, 708, 710, and 712 thecorresponding produce the focal points 714, 716, 718, 720, and 722 thatresult in the heating area 724. As a result, the predetermined distance728 is based on the design of the lens array assembly 700 because thefocal lengths are based on the design of the lens array sub-assembly700. The support structure 128 is configured to maintain thispredetermined distance 728 between the lens array assembly 700 and theheating area 724 within the heating container 726. As such, since thetype of material, thickness, position, and angle of the lens paneswithin each lens array sub-assemblies 704, 706, 708, 710, and 712determines the corresponding focal points 714, 716, 718, 720, and 722,it is appreciated that the type of material, thickness, position, andangle of the lens panes within each lens array sub-assemblies 704, 706,708, 710, and 712 may also be designed such that they produce thecorresponding focal points 714, 716, 718, 720, and 722 at thepredetermined distance 728.

Turning to FIG. 8, an alternative approach is shown. In FIG. 8, a systemview of SRD 800 is shown in accordance with the present disclosure. Inthis example, a center-line 802 is shown for equivalent lens 803 ofplurality of lens panes of the SRD 800 and the SRD 800 is shown to havea focal length 804 that extends to a focal point 806 past the bottom 808of the heating container 810. As an example of operation, the heatingcontainer 810 is full of industrial material 812 to be melted such as,for example, aluminum. The impinging diffuse solar energy 814 isrefracted by the plurality of lens panes of the SRD 800 to form aplurality of refracted solar beams 816 (also known as rays) that arefocused to focal point 806 past the bottom 808 of the heating container810. Since, the heating container 810 is full of aluminum 812 to meltthe focused refracted solar beams 816 cannot concentrate their combinedenergy at focal point 806 and instead impinge on the aluminum 812 at aheating plane 820 that may correspond to the fill line of the aluminum812 in the heating container 810. Since the heating plane 820corresponds to a heating area 822 at the opening 824 of the heatingcontainer 810, the resulting heat generated by the focused refractedsolar beams 816 is distributed over the heating area 822 which is arelatively small area compared to the size of the SRD 800. By properlydesigning the SRD 800, the heating area 822 receives the proper amountof energy from the SRD 800 to either properly heat or melt theindustrial material (in this example aluminum) 812 in the heatingcontainer. In general, since SRD 800 focus light with minimal energyloss, the highest intensity of light is in the center 826 but is morediffuse moving outwards from the center 826. As such, the highestintensity of heat in the heating plane 820 is at the center and thenlowers in intensity away from the center 826 resulting in effectiveheating area 822. As described earlier, the focal length 804 is relatedto the predetermined length 830 between the center-line 802 ofequivalent lens 803 to the heating container 810 where the predeterminedlength 830 is the length from the center-line 802 to the heating plane820 within the heating container 810.

In some melting cases, an individual SRD 800 may not be able to properlygenerate enough energy to properly melt an industrial material 812 in aheating container 810 or to melt enough quantity of the industrialmaterial 812 to be competitive with non-solar methods. In these cases,multiple SRDs may be utilized in a chain to increase the amount ofindustrial material to be melted, heat the industrial material instages, or both. In FIG. 9, a perspective back-view of a plurality ofSRDs 900, 902, 904, and 906 are shown in accordance with the presentdisclosure. In this example, the SRDs 900, 902, 904, and 906 areutilized to melt an industrial material 908 in a plurality of heatingcontainers 910, 912, 914, and 916, respectively. In this example, themultiple SRDs 900, 902, 904, and 906 may be positioned by any knownsolar tracking system to collect the optimal quantity of solar lightduring the day. To maintain the optimal energy focusing of the SRDs 900,902, 904, and 906, the heating containers 910, 912, 914, and 916 may bemoved from one SRD to the next via a track system 918. In this example,the track system 918 may be configured to input or extract a givenheating container 910, 912, 914, and 916 at any point during the heatingand melting process to remove melted or heated material and input newmaterials in new heating containers (not shown).

Turning to FIG. 10, a flowchart 1000 of an example process performed bythe SRD is shown in accordance with the present disclosure. In general,the process includes heating an industrial material within a heatingcontainer with the SRD. The method starts 1002 by, in step 1004,refracting impinging solar energy on the SRD through a lens arrayassembly having a plurality of lens array sub-assemblies and, in step1006, focusing the refracted solar energy onto a plurality of focalpoints, where each focal point corresponds to a lens array sub-assemblyof the plurality of lens array sub-assemblies. The method then, in step1006, creates a heating area within the heating container utilizing theplurality of focal points or focal lengths and then, in step 1008, heatsthe industrial material within the heating container at the heating areautilizing the focused refracted solar energy. The process then ends1010.

In FIG. 11, a flowchart 1100 of an example process performed infabricating the SRD is shown in accordance with the present disclosure.The process begins 1102 by determining the type and amount of industrialmaterial to be melted in step 1104. For example, if the application typemay include heating or melting aluminum, steel, or other metal,pre-heating or melting a non-metallic industrial material, heatingwater, heating, softening, or melting plastic. Once this is determined,the process (in step 1106) includes determining an amount of energyneeded to heat or melt the industrial material. As an example, to meltaluminum, the SRD needs to produce approximately 30,000 watts to meltabout 100 pounds of aluminum per hour. The process, in step 1108, thenincludes determining an array size for the lens array assembly forproducing the previously determined amount of energy, where the lensarray assembly is configured to refract solar light impinging on thelens array assembly to the industrial material. As an example, in Hawaiithe Sun produces about 1,000 watts per square meter so the lens arrayassembly needs to be approximately 30 m² (i.e., about 6 meters by 6meters). The process then, in step 1110, determines a focal length ofthe lens array assembly based on the geometry of the lens arrayassembly. The process, in step 1112, includes assembling the lens arrayassembly. The process then ends 1114. In this example, assembling thelens array assembly may also include assembling a plurality of lensarray sub-assemblies and attaching the plurality of lens arraysub-assemblies into the lens array assembly, where each lens arraysub-assembly has a corresponding focal length and wherein each lensarray sub-assembly has a convex shape. Assembling the lens arrayassembly may further include attaching a plurality of lens panes to eachplurality of lens array sub-assemblies, where the lens panes may includeFresnel lenses. Moreover, assembling the lens array assembly may alsoinclude a first lens array sub-assembly with a different correspondingfocal length than a second focal length corresponding to a second lensarray sub-assembly.

It is appreciated by those of ordinary skill in the art that while theprevious examples describe heating and melting industrial materials inheating container, the SRD may also be utilized to heat (and not melt)different types of materials for use in, for example, industrial boilersand electro-chemical processors where the energy provided by the SRD isused to heat intermediate materials such as water to produce steam thatmay be utilized for other processes such as powering turbines, heatingchemicals, or providing heat transfer for other types of heatingsystems.

Turning to FIG. 12, a system diagram of an example of an implementationof the SRD 1200 utilized for powering a turbine 1202 is shown inaccordance with the present disclosure. The turbine 1202 may include aplurality of turbine blades (also known as vanes) 1204 and a shaft 1206.In this example, the turbine 1202 is connected to a heating container1208 via at least an inflow tubular pipe 1210 and outflow tubular pipe1212. The heating container 1208 may have a plurality of heating pipes1214 within the heating container 1208 that are configured to be heatedby the SRD 1200. The heating pipes 1214 may be filled with a fluid suchas, for example, a gas (such as, for example, air), steam, water, orother heatable fluid that is capable of being heated in the heatingcontainer 1208 and passed to the turbine 1202 which is a rotary machinethat extracts the energy from the resulting fluid flow and converts itinto useful work energy that rotates 1216 the shaft 1206. In an exampleof operation, the SRD 1200 may receive solar energy and focus 1218 ittowards the heating pipes 1214 of the heating container 1208. As before,multiple focal points 1220, 1222, 1224, and 1228 may be focused 1218towards the heating container 1208 resulting in a heating area 1230along the heating container 1208. The fluid in the heating pipes 1214 isthen heated up and heated fluid 1232 passed to the turbine 1202 viainflow tubular pipe 1210. The heated fluid turns the turbine blades 1204resulting in the shaft 1206 rotating 1216 along its axis. The exhaustedfluid is returned to the heating container 1208 via the outflow tubularpipe 1212. It is appreciated by those of ordinary skill in the art thatother industrial heating examples may also be implemented by utilizingthe SRD 1200 as a heating device for other industrial materials.

It will be understood that various aspects or details of the inventionmay be changed without departing from the scope of the invention. It isnot exhaustive and does not limit the claimed inventions to the preciseform disclosed. Furthermore, the foregoing description is for thepurpose of illustration only, and not for the purpose of limitation.Modifications and variations are possible in light of the abovedescription or may be acquired from practicing the invention. The claimsand their equivalents define the scope of the invention.

What is claimed is:
 1. A method for heating contents in a containerusing a solar refraction device, the method comprising: refracting solarenergy impinging on a first surfaces of a lens array assembly of thesolar refraction device through the lens array assembly toward secondsurfaces of the lens array assembly, the lens array assembly having aplurality of lens array sub-assemblies; refracting the solar energy atthe second surfaces of the lens array assembly to focus refracted solarenergy at a plurality of focal points of the plurality of lens arraysub-assemblies, wherein each focal point corresponds to a lens arraysub-assembly of the plurality of lens array sub-assemblies; and creatinga heating area within the container with the refracted solar energy. 2.The method of claim 1, wherein the plurality of focal points are below abottom of the container.
 3. The method of claim 2, wherein the pluralityof lens array sub-assemblies have different focal lengths.
 4. The methodof claim 3, wherein the plurality of lens array sub-assemblies include aplurality of Fresnel lenses arranged on a curved frame of the lens arrayassembly.
 5. The method of claim 1, wherein the plurality of lens arraysub-assemblies are arranged on a curved frame of the lens array assemblysuch that light from multiple directions is focused through the lensarray sub-assemblies toward the container.
 6. The method of claim 1,wherein a curved frame is curved along at least two orthogonal axes. 7.The method of claim 1, wherein the plurality of focal points includesmultiple locations in the container.
 8. The method of claim 1, whereinthe contents are metals, non-metals, gasses or liquids.
 9. The method ofclaim 8, wherein the non-metals comprise plastics.
 10. A method forheating contents in a container using a solar refraction device, themethod comprising: refracting solar energy impinging on the solarrefraction device through a lens array assembly having a plurality oflens array sub-assemblies, wherein a first lens array sub-assembly ofthe plurality of lens array sub-assemblies has a substantially parabolicshape and is configured to maintain a plurality of lens panes arrangedin an array of columns and rows in a fixed relationship, and wherein thelens array assembly is configured to have a plurality of focal lengths;focusing refracted solar energy at a plurality of focal points with theplurality of lens array sub-assemblies, wherein each focal pointcorresponds to a lens array sub-assembly of the plurality of lens arraysub-assemblies; and creating a heating area within the container withthe refracted solar energy.
 11. The method of claim 10, furthercomprising moving the solar refraction device to track movement of thesun.
 12. The method of claim 10, further comprising moving the containerfrom a first location that receives the refracted solar energy from thesolar refraction device to a second location that receives secondrefracted solar energy from a second solar refraction device.
 13. Themethod of claim 10, further comprising: placing solid contents in thecontainer; and melting the solid contents in the container to a liquidphase with heat from the heating area.
 14. The method of claim 13,further comprising removing liquid phase material from the container.15. The method of claim 10, further comprising: placing liquid contentsin the container; and heating the liquid contents in the container. 16.The method of claim 10, wherein the contents are metals, non-metals,gasses or liquids.
 17. The method of claim 16, wherein the non-metalscomprise plastics.
 18. A method for fabricating a solar refractiondevice for heating industrial materials in a heating container having abottom, the method comprising: determining a first amount of energyneeded to melt or heat an amount of an industrial material; determiningan array size of a lens array assembly for focusing the first amount ofenergy, the array size based on the amount of the industrial material,wherein the lens array assembly is configured to refract solar lightimpinging on the lens array assembly to the industrial material;assembling a support frame to support the lens array assembly; andassembling the lens array assembly.
 19. The method of claim 18, furthercomprising: determining that the first amount of energy needed to meltor heat an amount of an industrial material exceeds a second amount ofenergy that a single solar refraction device can redirect; assemblingone or more additional lens array assemblies; and assembling a tracksystem to move the heating container to a first focus area associatedwith the lens array assembly and to second focus areas associated withthe one or more additional lens array assemblies.
 20. The method ofclaim 18, wherein assembling the lens array assembly includes:assembling a plurality of lens array sub-assemblies; and attaching theplurality of lens array sub-assemblies to the support frame, whereineach lens array sub-assembly has a corresponding focal length, andwherein each lens array sub-assembly has a convex shape.
 21. The methodof claim 20, wherein assembling the plurality of lens arraysub-assemblies includes attaching a plurality of lens panes to eachplurality of lens array sub-assemblies.
 22. The method of claim 21,wherein attaching the plurality of lens panes includes attaching aplurality of Fresnel lenses to each of the plurality of lens arraysub-assemblies.
 23. The method of claim 18, wherein the lens arrayassembly is shaped to form an approximate parabolic shape.
 24. Themethod of claim 23, wherein assembling a plurality of lens arraysub-assemblies further includes assembling a first lens arraysub-assembly with a different corresponding focal length than a secondfocal length corresponding to a second lens array sub-assembly.